Repository containing the files for the thesis : Optimization of an aircraft design problem for hybrid-electric configurations under manufacturing and certification constraints
Previously the control parameters from the mission were also used for landing. Not only did that prevent the investigating of different conrol scheme, it would also mean that if the control parameters were specified as array (of size 90, the size of the mission) it could not be used for landing (of size 3) which would cause the process to crash. It should not be the case anymore as these are two separate variables now.
Previously the control parameters from the mission were also used for landing. Not only did that prevent the investigating of different conrol scheme, it would also mean that if the control parameters were specified as array (of size 90, the size of the mission) it could not be used for landing (of size 3) which would cause the process to crash. It should not be the case anymore as these are two separate variables now.